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默认参数文件cfd_para.hypara更新

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hechao 2024-07-01 12:34:30 +08:00
parent 6cd9da73a0
commit 25aa6e302f
108 changed files with 4752 additions and 1080 deletions
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54
A01_TwoD_Plate_Laminar_Struct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A02_TwoD_Plate_Laminar_Ma5_Struct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A03_TwoD_plate_SST_LowMach_Struct/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A04_TwoD_Plate_SST_Ma5_Struct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A05_TwoD_Cylinder_Laminar_Ma8d03_Struct/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A06_ThreeD_NACA0012_SA_Struct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A07_TwoD_Rae2822_SST_Struct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A08_TwoD_30p30n_SST_Struct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A10_ThreeD_CHNT_SST_Struct_16CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A11_ThreeD_Sphere_Laminar_Ma10_Struct/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A12_ThreeD_DoubleEllipse_Laminar_Struct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A13_TwoD_BackwardStep_PressureOutlet_SA_Struct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A14_TwoD_Plate_TotalPressTempBC_SA_Struct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A15_ThreeD_ShockWave_PeriodicBoundary_SA_Struct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A16_TwoD_NLR7301_SST_Struct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A17_ThreeD_Compression_Ramp-16_SA_Struct/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A18_ThreeD_Hollow_Cylinder_Flare_Laminar_Struct_16CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A19_ThreeD_BluntCone_Ma10d6_Laminar_Struct_64CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A20_ThreeD_OV102_Ma20_Laminar_H50_Struct_24CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A21_ThreeD_ShockwaveInteractionPlate_Ma2_Laminar_UDB_Struct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A22_ThreeD_Jet_Ma3d33_SST_Struct_8CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A23_TwoD_Plate_S-KSR_SST_Struct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A24_TwoD_30p30n_SA_MatrixLUSGS_Struct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A25_TwoD_Plate_SST_LowMach_MatrixLUSGS_Struct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A26_TwoD_Rae2822_SA_MatrixLUSGS_Struct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
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@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A28_TwoD_Cylinder_Inv_Ma3d0_Entropyfix6_Struct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A29_TwoD_Rae2822_SA_Entropyfix6_Struct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A30_TwoD_Cylinder_Inv_Ma10d0_Entropyfix6_Struct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A31_ThreeD_CHNT_SST_MatrixLUSGS_Struct_256CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
A32_TwoD_NACA0012_Inv_Ma0d2_Precondition_Struct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B01_TwoD_NACA0012_SA_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B02_TwoD_NACA4412_SA_Unstruct_2CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B03_TwoD_Rae2822_SA_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B04_ThreeD_DLR-F6_SA_Unstruct_60CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B05_ThreeD_x38_Laminar_Unstruct_128CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B06_ThreeD_Axisymmetric_SA_Unstruct_64CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B07_ThreeD_Sphere_Laminar_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B08_TwoD_Plate_Laminar_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B09_TwoD_plate_SA_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B10_ThreeD_CompRamp-16_SA_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B11_ThreeD_DLR-GK01_Ma7_SA_Unstruct_8CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B12_ThreeD_DoubleEllipse_Laminar_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B13_ThreeD_Chnt_SA_Unstruct_100CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B14_TwoD_30p30n_SA_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B15_TwoD_NLR7301_SA_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B16_ThreeD_Hollow_Cylinder_Flare_Laminar_Unstruct_16CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B17_TwoD_Plate_S-KSR_SST_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B18_ThreeD_CRM-HL_Level-B_SA_Unstruct_1024CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B19_ThreeD_TrapWing_SA_AoA13_256CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B20_TwoD_NACA0012_SA_GMRES_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B21_ThreeD_Sphere_Laminar_GMRES_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B22_ThreeD_Rotor67_SngleZone_RotatingFrame_6CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B23_ThreeD_Stage35_MultiZone_MixingPlane_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B24_ThreeD_Aachen-row1_SngleZone_Periodicity_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B25_TwoD_Cylinder_Laminar_LowSpeed_Steady_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
B26_TwoD_Cylinder_Laminar_LowSpeed_Unsteady_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
C01_TwoD_Cylinder_Laminar_Mix_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
C02_TwoD_Rae2822_SST_Mix_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
C03_ThreeD_M6_SST_Mix_64CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
C04_ThreeD_F6-WB_SST_Mix_256CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
D01_TwoD_Cylinder_Laminar_HighOrder_Struct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
D02_ThreeD_DoubleEllipse_Laminar_HighOrder_Struct_48CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
D03_TwoD_30P30N_SST_HighOrderWENN_Struct_6CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
D04_ThreeD_ONERA_M6_SST_HighOrderWENN_Struct_8CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
D05_ThreeD_DoubleEllipse_Laminar_HighOrderWENN_Struct_48CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
E01_ThreeD_Cylinder_LES_Re3900_Struct_120CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
E02_ThreeD_Cylinder_LES_Re3900_Unstruct_120CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
E03-ThreeD_NACA0012_LES_Struct_400CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
F07-TwoD_NACA0012_PitchingMovement_SA_Struct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
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View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
F10-ThreeD_Brid_GridDeformationRBF_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
F11_ThreeD_M6_GridParallelRefine_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
F12_ThreeD_NRELPhaseⅥ_Laminar_OversetGrid_LowSpeed_Unsteady_Unstruct_64CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
G05_TwoD_Cylinder_N2-O2_Premixing-Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
G06_ThreeD_Sphere_N2-O2_Premixing-Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
H01_TwoD_BackStep_KE_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
H02_TwoD_Cavitity_Re100_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
H03_TwoD_GasLeakage_Steady_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
H04_TwoD_NACA0012_UPWIND_SA_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
H05_TwoD_NACA0012_SIMPLEC_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
H06_TwoD_NaturalConvection_CDS_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
H07_TwoD_Plate_Turb_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
H08_TwoD_Species_Turb_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
H09_ThreeD_Car_Turb_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
H10_ThreeD_Chnt_Lam_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
H11_ThreeD_GasLeakage_Unsteady_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
H12_ThreeD_Species_Transient_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
H13_ThreeD_SUBOFF_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

54
L01_TwoD_Cavity_BGK_MPI_1CPU/bin/cfd_para.hypara
View File

@ -295,6 +295,8 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -419,7 +421,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -513,6 +515,7 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number. // CFLMethod: The method to compute cfl number.
@ -521,6 +524,8 @@ double AusmpwPlusLimiter = 1.0;
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -569,7 +574,8 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -875,10 +881,7 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver.
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1054,9 +1057,6 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1155,7 +1155,6 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1424,6 +1423,41 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

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